Using Electrical Power Systems to Design a Rover

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I will talk about two topics in this discussion. The first being about important concepts that I discovered in the electrical power systems talk. This will include a discussion on the current battery of choice for the ISS and on protection systems for the SAWs (Solar Array Wings) against MMOD (Micrometeoroids and Orbital Debris). The second discussion topic will include how this information can possibly aid to the thought of designing a rover. The four key traits in this discussion are reliability, sustainability, life duration, and redundancy. You will find that the layout of this discussion is in order, as found below.

Topic I
I have to say that most of the topics covered I had previously discovered in the past, however I found it very interesting that the ISS uses Nickel-Hydrogen batteries. I never thought about the type of batteries the ISS used until now. The choice of this battery makes since, especially for when it was designed and constructed. Compared to other rechargeable batteries the NiH2 battery has a decently long life cycle of about 15 years or greater, and has a good specific energy. Furthermore the NiH2 has a great tolerance of overcharging and accidental reverse polarity. This are very key topics that must be considered when choosing a sustainable reusable battery. The only thing that concerns me with this choice is the harder more complex structure of the battery and a decrease (possibility) in safety. These batteries contain pressurized hydrogen gas up to 87 BAR. This means the housing must be rated for pressure, thus they are a bit more costly and more resource rich. Now as far of safety think of the Hindenburg accident, that was also hydrogen. Hydrogen gas can be very dangerous and it especially does not he...

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...reaction, thus giving off heat. To control the heat I would just use a potentiometer, allowing me to control the overall temperature of the electrical bay.
The ISS is an amazing station with an even more amazing electrical system onboard. Understanding its vast electrical layout really aids in the design of other electrical systems designed for space. In the future electrical systems will be redefined and vastly superior thus creating a greater potential for space exploration. In designing the electrical system for a Mars bound robot, there are many more considerations that must be made to increase the overall probability of success. However those were the four key traits that stuck out to me the most. I want to thank NASA for that webinar, it was very good and well thought out. I hope you enjoy my discussion and I look forward to hearing from everybody’s comments.

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